Airworthiness Directives (ADs)
CAA-2007-06-012A
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 2008/08/11
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Applicability
- AIRBUS A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aircraft, all manufacturer serial numbers.
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Model Number
- AIRBUS A318, A319, A320 and A321 aircraft
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CAA AD Number
- CAA-2007-06-012A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2008-0150
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Effective Date
- 2008/08/19
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Subject
- Flight Controls – Trimmable Horizontal Stabilizer Actuator (THSA) – Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 27; This AD supersedes EASA AD 2006-0223 dated 21 July 2006 and EASA AD 2007-0178 dated 22 June 2007; AIRBUS Service Bulletin A320-27-1164 Revision 6. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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Remarks
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